View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 21422U 26042.20098447 +.00000000 +00000-0 +17344-3 0 00004
2 21422 82.4961 109.2291 0013457 143.7779 216.4359 15.00004199 04
| Epoch (UTC): | 11 February 2026 04:49:25 |
| Eccentricity: | 0.0013457 |
| inclination: | 82.4961° |
| perigee height: | 558 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 109.2291° |
| argument of perigee: | 143.7779° |
| revolutions per day: | 15.00004199 |
| mean anomaly at epoch: | 216.4359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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